Simulation of the Transonic Truss-Braced Wing High-Lift Configuration at Mach 0.2 using USM3D-Mixed Element Solver
Year: 2025
Type: conference-paper
DOI: 10.2514/6.2025-3507
Institution: Langley Research Center
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4412485226
